View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 60365U 26144.88441512 +.00000000 +00000-0 +36790-4 0 00002
2 60365 53.1615 315.6655 0001321 82.7060 277.4091 15.31701056 03
| Epoch (UTC): | 24 May 2026 21:13:33 |
| Eccentricity: | 0.0001321 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 315.6655° |
| argument of perigee: | 82.7060° |
| revolutions per day: | 15.31701056 |
| mean anomaly at epoch: | 277.4091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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